Research Catalog

Reduction of helicopter blade-vortex interaction noise by active rotor control technology

Title
Reduction of helicopter blade-vortex interaction noise by active rotor control technology [microform] / Yung H. Yu ... [et al.].
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • Yu, Yung H.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TM ; 207568
Uniform Title
NASA technical memorandum ; 207568.
Alternative Title
Reduction of helicopter blade vortex interaction noise by active rotor control technology
Subject
  • Active control
  • Blade-vortex interaction
  • Control systems design
  • Smart structures
  • Structural design
  • Helicopters
  • Aircraft noise
  • Harmonic control
Note
  • Shipping list no.: 99-0199-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:207568
OCLC
marcive40771829
Title
Reduction of helicopter blade-vortex interaction noise by active rotor control technology [microform] / Yung H. Yu ... [et al.].
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA/TM ; 207568
NASA technical memorandum ; 207568.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Added Author
Yu, Yung H.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:207568
Research Call Number
READEX Microfiche NAS 1.15:207568
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